- Registered owner
- Rainier Heli International Inc
- Location
- Kirkland, WA
- Owner type
- Corporation
- Serial number
- 3691
- Year built
- 2003
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- May 22, 2003
- Certificate issued
- July 11, 2003
- Expires
- October 31, 2027
- Mode S code
- A07F81
Eurocopter EC 130 B4TCDS H9EUAirframe · Eurocopter EC 130 B4TCDS E00054ENEngine · Turbomeca ARRIEL-2B1
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 64
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2002 | 1 |
|---|---|
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 2 |
| 2006 | 2 |
| 2007 | 4 |
| 2008 | 3 |
| 2009 | 2 |
| 2010 | 7 |
| 2011 | 3 |
| 2012 | 4 |
| 2013 | 4 |
| 2014 | 6 |
| 2015 | 2 |
| 2016 | 2 |
| 2017 | 4 |
| 2018 | 2 |
| 2019 | 2 |
| 2020 | 5 |
| 2021 | 10 |
| 2022 | 3 |
| 2023 | 2 |
| 2024 | 1 |
| 2025 | 7 |
| 2026 | 7 |
Airframe · Eurocopter EC 130 B4
AD 2026-20-03Placards and MarkingsAD 2026-16-01Main rotor driveAD 2026-14-02Indication/Recording SystemInformation bulletins that may apply · 5
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N131GCMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Eurocopter EC 130 B4 aircraft
FAA incident reports
No FAA accident or incident reports matched to N131GCMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Eurocopter EC 130 B4 aircraft
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR PG9A115822Pump · wornPILOT REPORTED A SERVO AND HYD LIGHT ILLUMINATION DURING FLIGHT. UPON INSPECTION IT WAS FOUND, THAT THE SPLINES OF THE BELT DRIVEN HYD PUMP DRIVE COUPLING HAD WORN TO THE POINT THEY WERE SLIPPING. REPLACED HYD PUMP AND DRIVE COUPLING.SDR PG9A110603Pressure Switch · no testPRESSURE SWITCH PRODUCED NO INDICATION DURING TESTING./ REPLACED WITH SERVICEABLE PART.SDR PG9A108749Drive Shaft · wornFOUND LOOSE RIVETS AT THE AFT AND FORWARD END OF THE CENTER SECTION DRIVE SHAFT./ REPLACED SHAFT WITH NEW.SDR PG9A108314Windshield · crackedUPPER CENTER WINDSCREEN CRACKED WHILE SITTING ON THE RAMP. REPLACED THE WINDSCREEN WITH NEW.SDR PG9R118894Intake · crackedAIR INTAKE HAS A CRACK. (RMA NR R046894)SDR PG92004F00006Structure · crackedAIR INTAKE ASSEMBLY CRACKED. (RMA NR R045785) (K)
STCs that may be installed · 134
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 134 STCs